Method for forming three-dimensional structures with different material portions

ABSTRACT

A system and method for forming 3D printed structures includes one or more anchor portions on a base component. Additional materials can be printed on or adjacent to the anchor portions to provide additional structural components bonded to the anchor portions. These structures can be printed on, and can be a part of, a base component of an article of apparel.

CROSS REFERENCE TO RELATED APPLICATIONS

This application is a divisional of U.S. patent application Ser. No.16/375,804, filed Apr. 4, 2019, which is a divisional of U.S. patentapplication Ser. No. 15/590,966, filed May 9, 2017, now U.S. Pat. No.10,272,629, which is a divisional of U.S. patent application Ser. No.14/273,675, filed May 9, 2014, now U.S. Pat. No. 9,676,159. The priorapplications are incorporated herein by reference in their entirety.

BACKGROUND

The present embodiments relate generally to three-dimensional printingsystems and methods.

Three-dimensional printing systems and methods may be associated withvarious technologies including fused deposition modeling (FDM), electronbeam freeform fabrication (EBF), selective laser sintering (SLS) as wellas other kinds of three-dimensional printing technologies.

Structures formed from three-dimensional printing systems can be usedwith objects formed by other manufacturing techniques. These includetextile materials used in various articles of footwear and/or articlesof apparel.

SUMMARY

In one aspect, a method of manufacturing a structure for permanentattachment to a base component includes associating a first nozzle withthe base component, the first nozzle having a first aperture size. Themethod further includes forming an outer shell portion of the structureon the base component by extruding a first material through the firstnozzle, where the outer shell portion is formed with at least oneopening providing access to an interior of the outer shell portion. Themethod also includes removing the first nozzle from an area near theouter shell portion. The method also includes associating a secondnozzle having a second aperture size with the at least one opening,where the second aperture size is greater than the first aperture size.The method also includes extruding a second material through the secondnozzle and into the at least one opening in order to form an innerportion of the structure.

In another aspect, a method of manufacturing a structure for permanentattachment to a base component includes forming an outer shell portionof the structure on a surface of the base component by printing a firstmaterial onto the base component using a nozzle, where the outer shellportion is formed with at least one opening and where the outer shellportion is bonded to the base component. The method also includesfilling an interior of the outer shell portion by extruding a secondmaterial through the nozzle and into the at least one opening in orderto form an inner portion of the structure.

In another aspect, a method of manufacturing a structure for permanentattachment to a base component includes aligning a first nozzle with anopening in the base component, the nozzle being located adjacent to afirst side of the base component. The method further includes extrudinga first material through the opening and into a molding component on asecond side of the base component in order to form an anchored portionon the second side. The method also includes extruding the firstmaterial from the first nozzle on the first side to form an outer shellportion of the structure, where the outer shell portion is integrallyformed with the anchored portion and where the outer shell portionincludes an upper opening. The method further includes filling aninterior of the outer shell portion by extruding a second materialthrough a second nozzle and into the upper opening of the outer shellportion in order to form an inner portion of the structure.

Other systems, methods, features and advantages of the embodiments willbe, or will become, apparent to one of ordinary skill in the art uponexamination of the following figures and detailed description. It isintended that all such additional systems, methods, features andadvantages be included within this description and this summary, bewithin the scope of the embodiments, and be protected by the followingclaims.

BRIEF DESCRIPTION OF THE DRAWINGS

The embodiments can be better understood with reference to the followingdrawings and description. The components in the figures are notnecessarily to scale, emphasis instead being placed upon illustratingthe principles of the embodiments. Moreover, in the figures, likereference numerals designate corresponding parts throughout thedifferent views.

FIG. 1 is a schematic view of an embodiment of components of athree-dimensional printing system as well as several articles that maybe used with the three-dimensional printing system;

FIG. 2 is a schematic diagram of an embodiment of various sub-systemsassociated with a three-dimensional printing system;

FIG. 3 is a schematic diagram of an embodiment of a set of extrusioncontrol parameters;

FIG. 4 is a schematic diagram of an embodiment of a nozzle of athree-dimensional printing system and optional sensors;

FIG. 5 is a schematic view of an embodiment of a nozzle and a device formodifying physical properties of a portion of material recently ejectedfrom the nozzle;

FIG. 6 is a schematic isometric view of an embodiment of severalstructures that may be formed with a three-dimensional printing system;

FIGS. 7-14 are schematic views of steps in forming a knob-like structureby extruding material from a nozzle, according to an embodiment;

FIGS. 15-19 are schematic views of steps in forming a hook-likestructure by extruding material from a nozzle, according to anembodiment;

FIG. 20 is an embodiment of a process of adjusting the extrusion of amaterial according to information received from an optical device;

FIG. 21 is a schematic view of a process for sensing outward spreadingof a portion of a material and adjusting the flow rate of materialextruded from a nozzle in response, according to an embodiment;

FIG. 22 is an embodiment of a process of modifying the physicalproperties of a portion of extruded material;

FIGS. 23-27 are schematic views of steps in forming an anchoredstructure in a base component by extruding material from a nozzle,according to an embodiment;

FIG. 28 is a schematic view of an embodiment of several differentmolding components that may be used with a three-dimensional printingsystem;

FIG. 29 is a schematic view of an embodiment of a structure anchoredwithin a base component, in which portions of the structure extendthrough spaces in the material of the base component;

FIG. 30 is a schematic view of an embodiment of different configurationsfor associating portions of an article with a three-dimensional printingsystem;

FIG. 31 is a schematic isometric view of an embodiment of an article offootwear including various structures formed by a three-dimensionalprinting process;

FIG. 32 is a schematic view of an embodiment of a structure comprised ofdistinct materials, where each material is applied using a differentnozzle;

FIGS. 33-35 illustrate a schematic view of steps of forming a structureby forming an outer shell portion and then filling in the interior ofthe outer shell portion, where different nozzles are used for eachmaterial, according to an embodiment;

FIGS. 36-38 illustrate a schematic view of steps of forming a structureby forming an outer shell portion and then filling in the interior ofthe outer shell portion, where the same nozzle is used for eachmaterial, according to an embodiment;

FIG. 39 is a schematic view of an embodiment of a structure with anouter shell portion having at least two openings;

FIG. 40 is a schematic cross-sectional view of an embodiment of astructure with an outer shell portion anchored in a base component;

FIG. 41 is a schematic isometric exploded view of an embodiment of astructure with an outer shell portion anchored in a base component;

FIGS. 42-43 illustrate schematic views of steps of forming a structurewith an outer shell portion and an outwardly extending portion,according to an embodiment;

FIGS. 44-46 illustrate a schematic view of steps of forming a cleatmember with a base portion made of a first material and a tip portionmade of a second material;

FIG. 47 is a schematic isometric view of an embodiment of an article offootwear with a plurality of cleat members;

FIG. 48 is a schematic diagram of a nozzle control system including afirst nozzle and a second nozzle; and

FIG. 49 is an embodiment of a process for forming a structure with afirst nozzle and a second nozzle.

DETAILED DESCRIPTION

FIG. 1 is a schematic view of an embodiment of a three-dimensionalprinting system 100, also referred to simply as printing system 100hereafter. FIG. 1 also illustrates several exemplary articles 130 thatmay be used with printing system 100. Referring to FIG. 1, printingsystem 100 may further comprise printing device 102, computing system104 and network 106.

Embodiments may use various kinds of three-dimensional printing (oradditive manufacturing) techniques. Three-dimensional printing, or “3Dprinting”, comprises various technologies that are used to formthree-dimensional objects by depositing successive layers of material ontop of one another. Exemplary 3D printing technologies that could beused include, but are not limited to: fused filament fabrication (FFF),electron beam freeform fabrication (EBF), direct metal laser sintering(DMLS), electron beam melting (EMB), selective laser melting (SLM),selective heat sintering (SHS), selective laser sintering (SLS),plaster-based 3D printing (PP), laminated object manufacturing (LOM),stereolithography (SLA), digital light processing (DLP) as well asvarious other kinds of 3D printing or additive manufacturingtechnologies known in the art.

In the embodiments shown in the figures, printing system 100 may beassociated with fused filament fabrication (FFF), also referred to asfused deposition modeling. In the embodiment shown in FIG. 1, printingdevice 102 of printing system 100 uses fused filament fabrication toproduce three-dimensional parts. An example of a printing device usingfused filament fabrication (FFF) is disclosed in Crump, U.S. Pat. No.5,121,329, filed Oct. 30, 1989 and titled “Apparatus and Method forCreating Three-Dimensional Objects,” which application is hereinincorporated by reference and referred to hereafter as the “3D Objects”application. Embodiments of the present disclosure can make use of anyof the systems, components, devices and methods disclosed in the 3DObjects application.

Printing device 102 may include a housing 110 that supports varioussystems, devices, components or other provisions that facilitate thethree-dimensional printing of objects (e.g., parts, components,structures). Although the exemplary embodiment depicts a particularrectangular box-like geometry for housing 110, other embodiments coulduse any housing having any geometry and/or design. The shape and size ofthe housing of a printing device could be varied according to factorsincluding a desired foot-print for the device, the size and shape ofparts that may be formed within the printing device as well as possiblyother factors. It will be understood that the housing of a printingdevice could be open (e.g., provide a frame with large openings) orclosed (e.g., with glass or panels of solid material and a door).

In some embodiments, printing device 102 may include provisions toretain or hold a printed object (or a component supporting the printedobject). In some embodiments, printing device 102 may include a table,platform, tray or similar component to support, retain and/or hold aprinted object or an object onto which printed material is beingapplied. In the embodiment of FIG. 1, printing device 102 includes tray112. In some embodiments, tray 112 may be fixed in place. In otherembodiments, however, tray 112 could move. For example, in some cases,tray 112 may be configured to translate within housing 110 in ahorizontal direction (e.g., front-back and/or left right with respect tohousing 110) as well as a vertical direction (e.g., up-down withinhousing 110). Moreover, in some cases, tray 112 may be configured torotate and/or tilt about one or more axes associated with tray 112. Thusit is contemplated that in at least some embodiments, tray 112 may bemoved into any desired relative configuration with a nozzle or printhead of printing device 102.

In some embodiments, printing device 102 may include one or moresystems, devices, assemblies or components for delivering a printedmaterial (or printed substance) to a target location. As used herein,the terms “target location”, “target portion” or “target surface” referto any intended location, portion or surface where a printed materialmay be applied. Target locations could include the surface of tray 112,a surface or portion of a partially printed structure and/or a surfaceor portion of a non-printed structure or component. Provisions fordelivering printed materials include, for example, print heads andnozzles. In the embodiment of FIG. 1, printing device 102 includesnozzle assembly 116.

Nozzle assembly 116 may comprise one or more nozzles that deliver aprinted material to a target location. For purposes of clarity, theexemplary embodiment of FIG. 1 depicts a single nozzle 118 of nozzleassembly 116. However, in other embodiments, nozzle assembly 116 couldbe configured with any number of nozzles, which could be arranged in anarray or any particular configuration. In embodiments comprising two ormore nozzles, the nozzles could be configured to move together and/orindependently. For example, in an embodiment of a printing systemdiscussed below, a printing device could be configured with at least twonozzles that can move in an independent manner from one another.

Nozzle 118 may be configured with a nozzle aperture 119 that can beopened and/or closed to control the flow of material exiting from nozzle118. Specifically, the nozzle aperture 119 may be in fluid communicationwith a nozzle channel 121 that receives a supply of material from amaterial source (not shown) within printing device 102. In at least someembodiments, a filament of material (e.g., plastic or wire) is providedas a coil, which may then be unwound and fed through nozzle 118 to bedeposited at a target location. In some embodiments, a worm-drive may beused to push the filament into nozzle 118 at a specific rate (which maybe varied to achieve a desired volumetric flow rate of material fromnozzle 118). It will be understood that in some cases, the supply ofmaterial could be provided at a location near nozzle 118 (e.g., in aportion of nozzle assembly 116), while in other embodiments the supplyof material could be located at some other location of printing device102 and fed via tubes, conduits, or other provisions, to nozzle assembly116.

In some embodiments, nozzle assembly 116 is associated with an actuatingsystem 114. Actuating system 114 may include various components, devicesand systems that facilitate the motion of nozzle assembly 116 withinhousing 110. In particular, actuating system 114 may include provisionsto move nozzle assembly 116 in any horizontal direction and/or verticaldirection to facilitate depositing a material so as to form athree-dimensional object. To this end, embodiments of actuating system114 may include one or more tracks, rails, and/or similar provisions tohold nozzle assembly 116 at various positions and/or orientations withinhousing 110. Embodiments may also include any kinds of motors, such as astepper motor or a servo motor, to move nozzle assembly 116 along atrack or rail, and/or to move one or more tracks or rails relative toone another. In at least some embodiments, actuating system 114 mayprovide movement for nozzle assembly 116 in any of the x-y-z directionsdefined with respect to printing system 102 (e.g., Cartesiandirections).

It will be understood that for purposes of illustration, the components,devices and systems of printing device 102 are shown schematically inFIG. 1. It will therefore be appreciated that embodiments may includeadditional provisions not shown, including specific parts, componentsand devices that facilitate the operation of actuating system 114 andnozzle assembly 116. For example, actuating system 114 is shownschematically as including several tracks or rails, but the particularconfiguration and number of parts comprising actuating system 114 mayvary from one embodiment to another.

In different embodiments, printing device 102 may use a variety ofdifferent materials for forming 3D parts, including, but not limited to:thermoplastics (e.g., polyactic acid and acrylonitrile butadienestyrene), high density polyethylene, eutectic metals, rubber, clays(including metal clays), Room Temperature Vulcanizing silicone (RTVsilicone), porcelain, as well as possibly other kinds of materials knownin the art. In embodiments where two or more different printed orextruded materials are used to form a part, any two or more of thematerials disclosed above could be used.

As discussed above, printing system 100 can include provisions tocontrol and/or receive information from printing device 102. Theseprovisions can include a computing system 104 and a network 106.Generally, the term “computing system” refers to the computing resourcesof a single computer, a portion of the computing resources of a singlecomputer, and/or two or more computers in communication with oneanother. Any of these resources can be operated by one or more humanusers. In some embodiments, computing system 104 may include one or moreservers. In some cases, a print server may be primarily responsible forcontrolling and/or communicating with printing device 102, while aseparate computer (e.g., desktop, laptop or tablet) may facilitateinteractions with a user. Computing system 104 can also include one ormore storage devices including but not limited to magnetic, optical,magneto-optical, and/or memory, including volatile memory andnon-volatile memory.

In the exemplary embodiment of FIG. 1, computing system 104 may comprisea central processing device 185, viewing interface 186 (e.g., a monitoror screen), input devices 187 (e.g., keyboard and mouse), and softwarefor designing a computer-aided design (“CAD”) representation 189 of aprinted structure. In at least some embodiments, the CAD representation189 of a printed structure may include not only information about thegeometry of the structure, but also information related to the materialsrequired to print various portions of the structure.

In some embodiments, computing system 104 may be in direct contact withprinting device 102 via network 106. Network 106 may include any wiredor wireless provisions that facilitate the exchange of informationbetween computing system 104 and printing device 102. In someembodiments, network 106 may further include various components such asnetwork interface controllers, repeaters, hubs, bridges, switches,routers, modems and firewalls. In some cases, network 106 may be awireless network that facilitates wireless communication between two ormore systems, devices and/or components of printing system 100. Examplesof wireless networks include, but are not limited to: wireless personalarea networks (including, for example, Bluetooth), wireless local areanetworks (including networks utilizing the IEEE 802.11 WLAN standards),wireless mesh networks, mobile device networks as well as other kinds ofwireless networks. In other cases, network 106 could be a wired networkincluding networks whose signals are facilitated by twister pair wires,coaxial cables, and optical fibers. In still other cases, a combinationof wired and wireless networks and/or connections could be used.

In some embodiments, printed structures may be printed directly to oneor more articles. The term “articles” is intended to include botharticles of footwear (e.g., shoes) and articles of apparel (e.g.,shirts, pants, etc.). As used throughout this disclosure, the terms“article of footwear” and “footwear” include any footwear and anymaterials associated with footwear, including an upper, and may also beapplied to a variety of athletic footwear types, including baseballshoes, basketball shoes, cross-training shoes, cycling shoes, footballshoes, tennis shoes, soccer shoes, and hiking boots, for example. Asused throughout this disclosure, the terms “article of footwear” and“footwear” also include footwear types that are generally considered tobe nonathletic, formal, or decorative, including dress shoes, loafers,sandals, slippers, boat shoes, and work boots.

While the disclosed embodiments are described in the context offootwear, the disclosed embodiments may further be equally applied toany article of clothing, apparel, or equipment that includes 3Dprinting. For example, the disclosed embodiments may be applied to hats,caps, shirts, jerseys, jackets, socks, shorts, pants, undergarments,athletic support garments, gloves, wrist/arm bands, sleeves, headbands,any knit material, any woven material, any nonwoven material, sportsequipment, etc. Thus, as used throughout this disclosure, the term“article of apparel” may refer to any apparel or clothing, including anyarticle of footwear, as well as hats, caps, shirts, jerseys, jackets,socks, shorts, pants, undergarments, athletic support garments, gloves,wrist/arm bands, sleeves, headbands, any knit material, any wovenmaterial, any nonwoven material, etc. As used throughout thisdisclosure, the terms “article of apparel,” “apparel,” “article offootwear,” and “footwear” may also refer to a textile, a natural fabric,a synthetic fabric, a knit, a woven material, a nonwoven material, amesh, a leather, a synthetic leather, a polymer, a rubber, and a foam.

In an exemplary embodiment, printing device 102 may be configured toprint one or more structures directly onto a portion of one of articles130. Articles 130 comprise exemplary articles that may receive a printedstructure directly from printing device 102, including an article offootwear 132, which has a three-dimensional configuration, as well as anupper 134, which has a flattened configuration. Articles 130 alsoinclude t-shirt 136. Thus it will be understood that printing device 102may be used to apply printed material to articles in three-dimensionalconfigurations and/or flattened configurations.

In order to apply printed materials directly to one or more articles,printing device 102 may be capable of printing onto the surfaces ofvarious kinds of materials. Specifically, in some cases, printing device102 may be capable of printing onto the surfaces of various materialssuch as a textile, a natural fabric, a synthetic fabric, a knit, a wovenmaterial, a nonwoven material, a mesh, a leather, a synthetic leather, apolymer, a rubber, and a foam, or any combination of them, without theneed for a release layer interposed between a substrate and the bottomof the printed material, and without the need for a perfectly ornear-perfectly flat substrate surface on which to print. For example,the disclosed methods may include printing a resin, acrylic,thermoplastic material or ink material onto a fabric, for example a knitmaterial, where the material is adhered/bonded to the fabric and wherethe material does not generally delaminate when flexed, rolled, worked,or subject to additional assembly processes/steps. As used throughoutthis disclosure, the term “fabric” may be used to refer generally tomaterials chosen from any textile, natural fabric, synthetic fabric,knit, woven material, nonwoven material, mesh, leather, syntheticleather, polymers, rubbers, and foam.

Although some embodiments may use printing device 102 to printstructures directly onto the surface of a material, other embodimentsmay include steps of printing a structure onto a tray or release paper,and then joining the printed structure to an article in a separate step.In other words, in at least some embodiments, printed structures neednot be printed directly to the surface of an article.

Printing system 100 may be operated as follows to provide one or morestructures that have been formed using a 3D printing, or additive,process. Computing system 104 may be used to design a structure. Thismay be accomplished using some type of CAD software, or other kind ofsoftware. The design may then be transformed into information that canbe interpreted by printing device 102 (or a related print server incommunication with printing device 102). In some cases, the design maybe converted to a 3D printable file, such as a stereolithography file(STL file).

Before printing, an article may be placed onto tray 112. Once theprinting process is initiated (by a user, for example), printing device102 may begin depositing material onto the article. This may beaccomplished by moving nozzle 118 (using actuating device 114) to buildup layers of a structure using deposited material. In embodiments wherefused filament fabrication is used, material extruded from nozzle 118may be heated so as to increase the pliability of the material as it isdeposited.

Although some of the embodiments shown in the figures depict a systemusing filament fused fabrication printing technologies, it will beunderstood that still other embodiments could incorporate one or moredifferent 3D printing technologies. Moreover, still other embodimentscould incorporate a combination of filament fused fabrication andanother type of 3D printing technique to achieve desired results for aparticular printed structure or part.

FIG. 2 illustrates a schematic embodiment of a print control system 200.Referring to FIG. 2, print control system 200 includes an extrusioncontrol system 204, a sensor system 206 and a nozzle actuating system208. Each of these systems, discussed in further detail below, mayoperate in cooperation with one another to facilitate the printing of astructure. Specifically, nozzle actuating system 208 controls themovement of nozzle 118, while extrusion control system 204 controls theflow and properties of material deposited as nozzle 118 is moved around.Additionally, sensor system 206 includes provisions to provide feedbackto both nozzle actuating system 208 and extrusion control system 204 inreal-time, so that printing can be adjusted in real-time to achieveprecise geometries and material characteristics for printed structures.

Nozzle actuating system 208 allows for the motion of nozzle 118 in anydirection, including both horizontal and vertical directions withinhousing 110. In at least some embodiments, nozzle actuating system 208facilitates the motion of nozzle 118 along a tool path that isdetermined from the CAD design of the printed structure.

Extrusion control system 204 may include one or more provisions forcontrolling the flow of material from nozzle 118 (or any other nozzlesassociated with nozzle assembly 116) as well as the behavior of thematerial after it has been deposited onto a target location. As shownschematically in FIG. 3, extrusion control system 204 can be associatedwith one or more “extrusion control parameters” that can be varied tochange the flow rate of, and/or other properties of, the extrudedmaterial. For example, extrusion control parameters can include a nozzlewithdrawal rate 302, an extrusion rate 304, an extrusion temperature306, a nozzle diameter 308, an extrusion pressure 310, an ambienttemperature 312 and an ambient pressure 314. It will be understood thatthese parameters are only intended to be exemplary and other embodimentscould include additional extrusion control parameters. Also, in at leastsome embodiments, some of these extrusion control parameters may beoptional. In other words, in some other embodiments, one or more ofthese parameters may be either fixed or not adjustable.

Nozzle withdrawal rate 302 may characterize the rate at which nozzle 118is moved away from (or raised) an underlying surface where extrudedmaterial is being deposited. Because newly extruded material is forcedfrom nozzle 118 under pressure, changing the rate at which nozzle 118 ispulled away from the target location may tend to affect how the extrudedmaterial spreads on the target location. Extrusion rate 304 maycharacterize the rate at which material is flowing through aperture 121of nozzle 118. As used herein, the term “extrusion rate”, also referredto as the “flow rate”, refers to the volumetric flow rate at whichmaterial is extruded from (or flows from) the nozzle. Increasing theextrusion rate may tend to create a larger volume of material depositedat a given location over an interval of time, while decreasing theextrusion rate may tend to decrease the volume of material deposited ata given location for the same interval of time.

Extrusion temperature 306 may characterize the temperature of thematerial as it is extruded from nozzle 118 and deposited at a targetlocation. In at least some cases, varying the extrusion temperature maychange the pliability of the material, which can affect spreading of thematerial at the target location. Also, the temperature of the extrudedmaterial may affect how quickly the material cools and/or cures, whichcan also affect spreading and the final geometry of a printed structure.Nozzle diameter 308 characterizes the size of aperture 121 and/or ofchannel 123 of nozzle 118. Varying these diameters can affect the totalvolume of material deposited at a target location over a given period ofsame.

Extrusion pressure 310 characterizes the force per unit area applied bya portion of extruded material against a portion of material at a targetlocation. The extrusion pressure may affect the rate and degree ofspreading. Also, ambient temperature 312 and ambient pressure 314 maycharacterize the ambient temperature and ambient pressure, respectively,of the area near nozzle 118. In at least some embodiments, materialpliability and curing properties may vary significantly with differencesin ambient temperature and/or ambient pressure.

Embodiments can include provisions for adjusting one or more of theseextrusion control parameters. In some embodiments, for example, nozzlewithdrawal rate 302 may be controlled using actuating system 114, whichcontrols both the horizontal and vertical motions of nozzle 118.Additionally, some embodiments can include provisions to control aworm-drive or other mechanism that controls the extrusion rate 304and/or extrusion pressure 310 at which material is extruded from nozzle118. In some embodiments, the extrusion temperature 306 can becontrolled with heating coils 405 (see FIG. 4) within nozzle 118.Additionally, nozzle diameter 308 may be controlled using methods knownin the art. Finally, ambient temperature 312 and ambient pressure 314may be controlled with various different provisions known in the art forcontrolling temperature and pressure within a confined space. Of courseit will be understood that embodiments are not limited to theseexemplary provisions for controlling one or more extrusion controlparameters. Other embodiments could utilize any other systems, methodsand/or devices to control these various parameters that may be known inthe art.

It may be understood that the parameters discussed with respect toextrusion control system 204 are only intended to be examples ofparameters that may be used to control how material is deposited at atarget location such that the material behaves in the desired manner(e.g., spreads at a desired rate and cures at a desired rate). The typesof parameters used may depend on manufacturing considerations as well asthe specific design of the printing device. In an exemplary embodiment,printing device 102 may be designed to allow for the adjustment of atleast one the extrusion control parameters discussed here. In otherwords, in an exemplary embodiment, printing device 102 is designed sothat various extrusion control parameters may be adjusted in real-timeusing information provided as part of, or in coordination with, a 3Dprinting file for printing device 102.

FIG. 4 illustrates a schematic configuration of various sensors that maycomprise part of sensor system 206. Referring to FIG. 4, sensor system206 may include an ambient temperature sensor 410 and a nozzletemperature sensor 412. In this exemplary configuration, ambienttemperature sensor 410 may be located near, but not within or on, nozzle118. It will be understood that ambient temperature sensor 410 could beany kind of sensor known in the art for detecting information related toambient temperature. In the exemplary configuration shown in FIG. 4,nozzle temperature sensor 412 is disposed within nozzle 118. In somecases, nozzle temperature sensor 412 could be in direct contact withmaterial flowing through channel 121 of nozzle 118. In otherembodiments, however, nozzle temperature sensor 412 could be located inany other portion of nozzle 118, as well as possibly being mountedoutside of nozzle 118. In at least some embodiments where thetemperature of a flowing material is not directly measured, thetemperature of one or more parts of nozzle 118 may be used as a proxyfor the temperature of the material. It will be understood that nozzletemperature sensor 412 may generally be any kind of temperature sensorknown in the art.

Embodiments may also include provisions for detecting ambient pressure.In some embodiments, sensor system 206 may include ambient pressuresensor 414. Generally, ambient pressure sensor 414 may be any kind ofpressure sensing device known in the art.

Embodiments can include provisions for detecting optical informationabout a printed structure, including recently extruded material. In someembodiments, sensor system 206 includes an optical sensing device 416.Optical sensing device 416 may be any kind of device capable ofcapturing image information. Examples of different optical sensingdevices that can be used include, but are not limited to: still-shotcameras, video cameras, digital cameras, non-digital cameras, webcameras (web cams), as well as other kinds of optical devices known inthe art. The type of optical sensing device may be selected according tofactors such as desired data transfer speeds, system memory allocation,desired temporal resolution for viewing a printed structure, desiredspatial resolution for viewing a printed structure as well as possiblyother factors. In at least one embodiment, optical sensing device couldbe an image sensor having a minimal form factor, for example an opticalsensing device with a CMOS image sensor with a footprint on the order ofseveral millimeters or less.

Exemplary image sensing technologies that could be used with opticalsensing device 416 include, but are not limited to: semiconductorcharge-coupled devices (CCD), complementary metal-oxide-semiconductor(CMOS) type sensors, N-type metal-oxide-semiconductor (NMOS) typesensors as well as possibly other kinds of sensors. The type of imagesensing technology used may vary according to factors includingoptimizing the sensor type compatible with ambient conditions inprinting device 102 (and near or within nozzle 118), size constraints aswell as possibly other factors. In some other embodiments, opticalsensing devices that detect non-visible wavelengths (including, forinstance, infrared wavelengths) could also be used.

In different embodiments, the location of optical sensing device 416could vary. In some embodiments, for example, optical sensing device 416could be disposed near, or even attached to, nozzle 118. As nozzle 118is moved, optical sensing device 416 may therefore travel with nozzle118. In other embodiments, optical sensing device 416 could be disposedaway from nozzle 118. In some cases, optical sensing device 416 couldhave a fixed location and/or orientation relative to housing 110. Inother cases, optical sensing device 416 could have an adjustablelocation and/or orientation and could be movable independently of nozzle118.

Optical sensing device 416 may convert optical images into informationtransmitted via electrical signals to one or more systems of printingsystem 100. Upon receiving these electrical signals, the one or moresystems can use this information to determine a variety of informationabout objects that may be visible to optical sensing device 416.

Embodiments may include an electronic control unit 450, also referred toas ECU 450, for controlling and/or communicating with various sensors ofsensor system 206. For purposes of clarity, only a single ECU isdepicted in this embodiment. However, it will be understood that inother embodiments multiple ECU's could be used, each ECU communicatingwith some or all of the sensors. The ECU's may themselves be furtherassociated with a particular system or device of printing system 100.

ECU 450 may include a microprocessor, RAM, ROM, and software all servingto monitor and control various components of sensor system 206, as wellas other components or systems of printing system 100. For example, ECU450 is capable of receiving signals from numerous sensors, devices, andsystems associated with printing system 100. The output of variousdevices is sent to ECU 450 where the device signals may be stored in anelectronic storage, such as RAM. Both current and electronically storedsignals may be processed by a central processing unit (CPU) inaccordance with software stored in an electronic memory, such as ROM.

ECU 450 may include a number of ports that facilitate the input andoutput of information and power. The term “port” as used throughout thisdetailed description and in the claims refers to any interface or sharedboundary between two conductors. In some cases, ports can facilitate theinsertion and removal of conductors. Examples of these types of portsinclude mechanical connectors. In other cases, ports are interfaces thatgenerally do not provide easy insertion or removal. Examples of thesetypes of ports include soldering or electron traces on circuit boards.

All of the following ports and provisions associated with ECU 450 areoptional. Some embodiments may include a given port or provision, whileothers may exclude it. The following description discloses many of thepossible ports and provisions that can be used, however, it should bekept in mind that not every port or provision must be used or includedin a given embodiment.

As indicated in FIG. 4, ECU 450 includes port 451 for communicatingwith, and/or powering, ambient pressure sensor 414. ECU 450 alsoincludes port 452 for communicating with, and/or powering, ambienttemperature sensor 410; port 453 for communicating with, and/orpowering, nozzle temperature sensor 412; and port 454 for communicatingwith, and/or powering, optical sensing device 416.

FIG. 4 also schematically indicates optional heating coils 405associated with nozzle 118 that may be used to heat nozzle 118 and/ormaterial flowing through nozzle 118. Heating coils 405 may be connectedto ECU 450, or a similar control unit. Although the exemplary embodimentdepicts heating coils disposed interior to nozzle 118, other embodimentscould use heating coils at any other portion nozzle assembly 116, aswell as possibly other portions of printing device 102 upstream ofnozzle assembly 116. It will also be understood that heating coils areonly one exemplary type of heating device that could be used. Otherembodiments could utilize any other heating devices, systems ormechanisms known in the art for heating nozzles, valves, channels, tubesor other systems associated with the transfer of a flowing material.

Embodiments can include provisions to control the properties of amaterial that has been recently extruded or deposited from a nozzle. Inat least some embodiments, printing device 102 may include one or morecuring control devices. A curing control device may be any device thatallows for the curing of the extruded material to be controlled, oradjusted, after the material has been extruded from a nozzle.

FIG. 5 is a schematic view of an embodiment of two curing controldevices 500. Curing control devices 500 includes a cooling device 502and a UV lighting device 504. Cooling device 502 may be a device thatapplies cooled air (i.e., air well below ambient temperature) to aportion of extruded material 520. The application of cooled air mayfacilitate faster curing of the portion of extruded material 520.Likewise, UV lighting device 504 may be a device that appliesultraviolet radiation to a portion of extruded material 522. Formaterials that may be UV cured, the application of ultraviolet light mayfacilitate faster curing of the portion of extruded material 522.Although not shown, it is also contemplated that some embodiments couldincorporate one or more heating devices that allow portions of extrudedmaterial to be heated above the temperature at which they are extruded,in order to temporarily increase pliability and flow, so that thematerial may more quickly spread over a target location.

Although a single device is shown for each kind of curing control devicein the exemplary embodiment of FIG. 5, other embodiments could includetwo or more of each kind of curing control device. Moreover, someembodiments could include single devices that provide coverage (e.g.,application of cooled air or UV radiation) through a wide range ofangles surrounding the extruded portion of material. Such embodimentscould apply cooled air and/or UV radiation to regions ranging from a fewdegrees to 360 degrees around the portion of extruded material.

It is contemplated that curing control devices could be applied locallyor globally. For example, in FIG. 5, both curing control devices 500 arecomprised of a relatively narrow probe-like device that applies cooledair and/or UV radiation to a local portion of extruded material.However, other embodiments could include larger devices that applycooled air and/or UV radiation to a large portion, or even all portionsof, extruded material. Still further, some embodiments may use curingcontrol devices 500 to provide local curing to predetermined portions ofa structure while the structure is printed, and may also use additionalcuring provisions to provide curing to the entire structure after theprinting process has been completed. For example, in another embodiment,following the formation of a printed structure, the entire printedstructure could be exposed to cool air and/or UV radiation for curing.

Embodiments that use highly local applications of cooled air and/or UVcuring (or possibly heating), may help improve the precision of forminga three-dimensional structure. For example, applying cooled air to somethermoplastic materials may allow the extruded material to be cured veryquickly, thereby allowing for improved precision in forming curvedand/or overhanging structures in relatively short periods of time.Additionally, because the exemplary embodiments contemplate extrudingrelatively large volumes of material at a target location in a shortperiod of time compared to some alternative methods, decreasing curingtime of the material as it is extruded using curing control devices canhelp improve the overall quality of the printed structure.

FIG. 6 is a schematic isometric view of an embodiment of several 3Dprinted structures 600, also referred to simply as structures throughoutthis detailed description and in the claims. Structures 600 include anexemplary cleat structure 602, hook structure 604 and knob-likestructure 606. It will be understood that these structures are onlyintended to be examples of possible 3D printed structures that can beformed using the methods disclosed herein. Moreover, in at least someembodiments, these exemplary structures may be formed using an extrusiontype of 3D printing process that can decrease total printing times oversome other embodiments of 3D printing methods.

In the embodiment shown in FIG. 6, structures 600 are bonded to basecomponent 610. Base component 610 is shown schematically for purposes ofillustration, and could be considered to be a portion of various kindsof articles including both articles of footwear and articles of apparelin some embodiments. As used throughout this detailed description and inthe claims, a “base component” may generally comprise any component thatto which one or more printed structures have been applied. A basecomponent could be a textile material (including woven textiles, knittextiles, braided textiles and non-woven textiles), a leather (naturalor synthetic) a plastic (including a plastic film), rubber, a metal orany other kind of material. Furthermore, in some embodiments 3D printedstructures could be printed directly onto the surface of a basecomponent. In such embodiments, the one or more materials forming the 3Dprinted structure may be bond compatible with at least one material ofthe base component. In other embodiments, the one or more materialsforming the 3D printing structure could be applied to the base componentafter printing, for example, using an adhesive or a mechanicalconnection.

FIGS. 7-14 illustrate schematic views of an embodiment of a process forforming 3D printed structure 606 (a knob-like structure) on basecomponent 610. The formed structure 606 is shown specifically in FIG.14. For purposes of description, several terms are defined herein torefer to material used in forming a 3D printed structure, includingterms indicating various states or configurations of material throughoutthe forming process. The term “portion of material” is used herein torefer to any volume or part of an extruded material that may or may notbe continuous with adjacent volumes or parts of extruded material. Aportion of material may be located exterior to a nozzle (once theportion has been extruded or deposited) or may be located interior tothe nozzle (or even upstream of the nozzle) prior to extrusion. Stillfurther, a portion of material can be partially disposed within thenozzle and partially exterior to the nozzle. Once extruded and cured(e.g., hardened), portions of material may comprise portions of thefinal 3D printed structure.

As previously described, a material 700 is extruded through and fromnozzle 118. The material exiting nozzle 118 may be characterized hereinas being “extruded”, “printed”, “ejected” or “deposited”. Material 700could comprise any kind of printable and/or extrudable material.Different embodiments could use materials including, but not limited to:an ink, a resin, an acrylic, a polymer, a thermoplastic material, athermosetting material, a light-curable material, or combinationsthereof. Some embodiments could also utilize filler materialsincorporated into an extruded or printed material. For example, a fillermaterial incorporated into an extruded material may be a powderedmaterial or dye designed to impart desired color or color patterns ortransitions, metallic or plastic particles or shavings, or any otherpowdered mineral, metal, or plastic. In at least some embodiments,therefore, material 700 may thus be a composite material. In oneembodiment, material 700 may be a thermoplastic material that may beheat cured (i.e., heated above its glass transition temperature forprinting and then cooled to form a relatively rigid, or non-pliable,printed structure).

For purposes of consistency and convenience, a first direction 702(shown schematically in FIG. 7) is defined relative to nozzle 118. Firstdirection 702 is a direction extending along a central axis of nozzle118 and defines an “extruding direction”, i.e., a direction along whichmaterial is extruded from, or pushed from, nozzle 118. In embodimentswhere nozzle 118 is primarily kept in a fixed orientation and raisedvertically away from base component 610, first direction 702 may remainapproximately perpendicular with an outer surface 611 of base component610, as depicted in the embodiment of FIGS. 7-14. However, in otherembodiments where the orientation of nozzle 118 may change with respectto a base component, as shown in the embodiment of FIG. 19, firstdirection 702 may be characterized as remaining approximately parallelwith a central axis of the formed 3D printed structure such that nozzle118 is always extruding material onto the end, or most recently formed,portion of the structure.

A second direction 704 is characterized as a direction that isapproximately perpendicular to first direction 702. Although shown inthe embodiments as oriented in a particular widthwise direction, itshould be understood that second direction 704 is representative of anydirection perpendicular to first direction 702. For example, seconddirection 704 may be characterized as a radial direction with respect tofirst direction 702. In some cases, first direction 702 may becharacterized as an axial direction. In embodiments where nozzle 118 isprimarily kept in fixed orientation with respect to base component 610,as in the embodiment of FIGS. 7-14, second direction 702 may beapproximately parallel with outer surface 611 of base component 610.However, in embodiments where the orientation of nozzle 118 may changerelative to a base component, as shown in FIG. 19, second direction 704may still be characterized as being perpendicular to first direction702, and may generally be approximately parallel with a lateral orwidthwise direction of a portion of a structure adjacent to nozzle 118.

The exemplary embodiment contemplates “extruding” (i.e., thrusting orpushing) portions of material through the nozzle, which may generateforces and pressures within the material initially directed along firstdirection 702. As portions of material exit nozzle 118, however, contactwith base component 610 and/or portions of material already formed onbase component 610 may result in a change of flow direction from beingprimarily along first direction 702, to being primarily along seconddirection 704. In other words, when pushed against either base component610 or an adjacent portion of material, the recently extruded portionsof material may tend to flow, or spread, outwardly along seconddirection 704. This flow may be alternatively characterized as “outwardspreading” as it tends to occur in a direction that is radially outwardfrom the initial stream of material extruded from nozzle 118 in firstdirection 702. In embodiments where a structure is formed with alongitudinal axis oriented in first direction 702, this outwardspreading may be oriented along a lateral dimension (or widthwise)dimension of the 3D printed structure.

For purposes of characterizing the dimensions of portions of materialoriented in second direction 704, the term “cross-sectional area” isused to refer to the cross-sectional area of a portion of material takenalong second direction 704. In particular, the cross-sectional area isgenerally taken through a plane that is (like second direction 704)perpendicular to first direction 702. In at least some embodiments, theportions of material may spread uniformly outwardly in the seconddirection 704, so that the cross-sectional area is approximatelycircular. In such cases, the term “diameter” may also be used tocharacterize the dimensions of the portion of material oriented alongsecond direction 704. In particular, any approximately circularcross-sectional area for a portion may have a unique correspondingdiameter.

As shown in FIGS. 7-14, in the exemplary printing process, material 700is extruded from nozzle 118 onto base component 610. In FIGS. 7 and 8, afirst portion of material 710 is extruded directly onto outer surface611 of base portion 610. As nozzle 118 is raised from a position indirect contact with base component 610 (FIG. 7) to a position disposed adistance 750 from base component 610 (FIG. 8), first portion of material710 undergoes spreading in second direction 704. As material 700 iscontinually extruded from nozzle 118, first portion of material 710expands from having a first cross-sectional area 720 (FIG. 8) to havinga second cross-sectional area 722 (FIG. 9), which is larger than firstcross-sectional area 720. In this case, since the approximate distanceof nozzle 118 to base component 610 is unchanged between theconfiguration of FIG. 8 and the configuration of FIG. 9, first portionof material 710 retains an approximately constant height and the outwardflow of material can be seen to be partially due to the constriction offirst portion of material 710 between the end of nozzle 118 and basecomponent 610.

Moving next to the configuration shown in FIG. 10, first portion ofmaterial 710 may stop spreading in second direction 704 as first portionof material 710 is cured (by cooling below a predetermined temperatureor another mechanism) and as nozzle 118 is raised to a position a seconddistance 752 from base component 610. Here, first portion of material710 has formed a first portion of structure 606, as seen by comparingthe geometry of first portion of material 710 in FIG. 14 with acorresponding first portion 740 of structure 606 shown in FIG. 10. Asseen in FIG. 10, a second portion of material 712, generally continuouswith first portion of material 710, is extruded from nozzle 118 ontofirst portion of material 710. Being pushed down against first portionof material 710, and partially constricted between nozzle 118 and firstportion of material 710, second portion of material 712 spreadsoutwardly in second direction 704.

In the next configuration of the process shown in FIG. 11, secondportion of material 712 has spread until second portion 742 of structure606 has been formed, as seen by comparing FIGS. 11 and 14. Together,first portion 740 of structure 606 and second portion 742 of structure606, formed by first portion of material 710 and second portion ofmaterial 712, respectively, comprise a bottom most portion of structure606 with a generally increasing cross-sectional area (and diameter) fromfirst portion 740 to second portion 742. Correspondingly, in theconfiguration indicated in FIG. 11, second portion of material 712 has alarger cross-sectional area 724 than the cross-sectional area 722 offirst portion of material 710. Here it may be understood that thecross-sectional areas of each portion varies through the height of eachportion so that cross-sectional area 724 and cross-sectional area 722are only representative cross-sectional areas.

As indicated in FIG. 11, the contact angle 790 with respect to outersurface 611 for the portion of structure 606 formed by first portion ofmaterial 710 and second portion of material 712 is greater than 90degrees. In an exemplary embodiment, contact angle 790 may be in therange between 120 and 160 degrees. Such large contact angles allow for awider variety of part geometries, with both convex and concave portionsbeing configurable at the bottom-most layer of the structure to enhancedesign and in some cases functionality of the structure.

In the configuration shown in FIG. 12, a third portion of material 714has been extruded onto second portion of material 712. Furthermore, afourth portion 716 of material 700 has been extruded onto third portionof material 714. Here, third portion of material 714 has across-sectional area 726 that is substantially greater than across-sectional area 728 of fourth portion of material 714.

At this stage, in some embodiments, curing control devices 500 may beapplied to increase the speed at which third portion of material 714and/or fourth portion of material of material 716 are cured. This mayhelp ensure that these portions are stable enough to support additionalextruded material on top of fourth portion of material 716, and toensure these portions are cured before their geometries are distorteddue to material flow under gravity. In an embodiment where material 700is a thermoplastic material, curing control devices 500 could be coolingdevices that supply cooled air below a predetermined temperature(associated with hardening) to local areas of structure 606 (i.e., areascorresponding to first portion of material 714 and/or second portion ofmaterial 716). Once hardened, third portion of material 714 and fourthportion of material 716 correspond to a third portion 744 and a fourthportion 746 of structure 606.

In FIG. 13, a fifth portion of material 718 is extruded onto fourthportion of material 716 to form a fifth portion 748 of structure 606that comprises the top-most portion of structure 606. As indicated inFIG. 13, fifth portion of material 718 has a cross-sectional area 729that is substantially greater than the cross-sectional area 728 offourth portion of material 716.

Once completed, nozzle 118 stops extruding material and pulls away fromthe formed structure 606 shown in FIG. 14. As seen in FIG. 14,corresponding to the varying cross-sectional areas of the portions ofmaterial used to form structure 606, different portions of structure 606have different cross-sectional areas. For example, a bottom portion ofstructure 606, which includes first portion 740, second portion 742 andthird portion 744, has a representative cross-sectional area 735. Fourthportion 746, forming the middle of structure 606, has a representativecross-sectional area 733, which is less than cross-sectional area 735.Finally, a top portion of structure 606, comprised of fifth portion 748of structure 606, has a cross-sectional area 731, which is greater thancross-sectional area 733. Thus, it may be seen that this process allowsfor the formation of structures that vary in cross-sectional geometryfrom bottom to top, including structures that go from wide, to narrow towide again. Moreover, this exemplary process could be used to formprinted structured having different portions with any combinations ofvariable cross-sectional areas.

Generally, the formation of portions having different cross-sectionalareas may be achieved by varying one or more extrusion controlparameters throughout the formation of a 3D printed structure. Asalready discussed, the amount of spreading of material in the seconddirection (also referred to as “outward spreading”) is due to variousfactors including flow rate, temperature (related to materialviscosity), constriction forces between the nozzle and an underlyingportion of material (or base component), as well as other factors.Therefore, adjusting one or more of these parameters throughout theprinting of a 3D structure will result in portions of varying outwardspread, and therefore varying cross-sectional areas (or diameters).

In order to illustrate an exemplary method for varying an extrusionparameter in the process shown in FIGS. 7-14, a flow rate parameter isindicated schematically in each of FIGS. 7-14 by an arrow oriented alongfirst direction 702. In particular, the magnitude of the flow rate atvarious stages in the printing process is depicted by variations inarrow length (with shorter arrows indicating relatively slower flowrates and longer arrows indicating relatively faster flow rates). Asseen in FIGS. 7-13, the flow rate may generally vary according to thedesired cross-sectional area or diameter of a portion. For example, inFIGS. 8-9, the flow rate 780 of material 700 is relatively slow comparedto a faster slow rate 782 of material 700 shown in FIGS. 10 and 11. Thisincrease in flow rate may result in a slightly larger cross-sectionalarea for second portion of material 712 compared to the cross-sectionalarea of first portion of material 710, as more material is laid down forthe same duration of time. As third portion of material 714 is extruded,the flow rate of material 700 is slower than flow rate 782, to create asmaller cross-sectional area for the corresponding portion of structure606. As shown in FIG. 12, as fourth portion of material 716 is extruded,the flow rate 784 may obtain a minimum value compared to other flowrates occurring during the process, as fourth portion 716 (correspondingto fourth portion 746 of structure 606) has the smallest cross-sectionalarea of all portions of structure 606. Finally, to achieve a graduallyincreased cross-sectional area for fifth portion of material 718, flowrate 786 is increased again relative to flow rate 784.

For purposes of clarity, the embodiments depict changes in the flow rateof material 700 as a primary way of controlling the resulting diameterof a formed portion for structure 606. However, it will be understoodthat any other extrusion control parameters could also be varied,possibly in combination with other extrusion control parameters. Forexample, another means for controlling the degree of outward spreadingof material is the nozzle withdrawal rate, since the constriction ofmaterial between the end of the nozzle and underlying material can be afactor in the degree of outward spreading. Thus, for example, formingrelatively narrow portions of a structure, such as third portion 744 ofstructure 606, could be accomplished by increasing the nozzle withdrawalrate so that material is built up vertically with less outwardspreading. In at least some embodiments, third portion 744 could beformed with an increased nozzle withdrawal rate (relative to the nozzlewithdrawal rate used for forming other portions) and a reduced flow rate(relative to the flow rates used for forming other portions).

Still other embodiments could use variations in nozzle temperature (aproxy for material temperature), ambient temperature, ambient pressureas well as any other extrusion control parameters to vary the geometry(e.g., cross-sectional area) of different portions and/or other materialcharacteristics of different portions (e.g., density, hardness, etc.).

As seen in FIGS. 7-14, this exemplary embodiment may use a fixed nozzlecross-sectional area 760 for extruding material 700. Moreover,cross-sectional area 760 is seen to be substantially smaller than thecross-sectional areas of various portions of structure 606. For example,cross-sectional area 760 is substantially less than cross-sectional area733 of third portion 716 of structure 606, which is the narrowestportion of structure 606. In still other embodiments, of course, thecross-sectional area (or diameter) of nozzle 118 could be varied toincrease (or decrease) the flow rate of material 700.

The exemplary process shown in FIGS. 7-14 may be useful in improving thespeed of forming 3D printed structure 606. Specifically, when comparedto methods used in other embodiments, where a structure is formed bymoving nozzle 118 to form horizontal layers and vertically to buildsubsequent layers on existing layers, this exemplary process may providesubstantially decreased printing times. This may occur since alternativeembodiments require a nozzle to move through a path that corresponds tothe entire volume of the desired 3D printed part, while the exemplarymethod may hold the nozzle at a fixed horizontal location and useoutward spreading of the material to fill out the intended 3D volumewithout requiring the nozzle to pass over every horizontal locationwhere material is to be located in the final structure.

FIGS. 15-19 illustrate another embodiment of a process of forming a 3Dprinted structure from a material 800. Referring to FIGS. 15-19, 3Dprinted structure 604, comprising a hook or hook-like fastener, isformed using a similar extrusion process described above and shown inFIGS. 7-14. However, in contrast to the embodiment of FIGS. 7-14, theprocess of FIGS. 15-19 includes moving nozzle 118 in more than just asingle direction (e.g., a vertical direction) away from a basecomponent. In particular, as described herein, nozzle 118 may be movedin two approximately perpendicular directions (e.g., a verticaldirection and a horizontal direction) to form structure 604.

Starting with FIG. 15, nozzle 118 extrudes a first portion of material802 to form a base portion of structure 606, which is bonded to basecomponent 610. Next, as shown in FIG. 16, nozzle 118 is raised in afirst direction 830, for example, a vertical direction, as secondportion of material 804 is extruded. As shown in a subsequentconfiguration in FIG. 17, in order to form a curved portion forstructure 604, nozzle 118 may be moved in both the first direction 830and a second direction 832 (e.g., a horizontal direction), as thirdportion of material 806 is extruded from nozzle 118. Moreover, in atleast some embodiments, curing control device 500 may be applied tothird portion of material 806 to decrease curing time so that thirdportion of material 806 maintains a desired curved and overhanginggeometry against the force of gravity that may otherwise cause material800 to flow down. In FIG. 18, nozzle 118 continues to form a curvedportion for structure 604, as fourth potion of material 808 is extrudedwhile nozzle 118 moves in both the first direction 830 and the seconddirection 832.

In at least some embodiments, nozzle 118 may be capable of changing itsorientation with respect to another component or part, such as basecomponent 610. As shown in FIG. 19, in one embodiment, nozzle 118 can berotated by an angle 850 so that nozzle 118 is no longer oriented in anapproximately perpendicular manner to base component 610. Instead,nozzle 118 may be oriented so that extruded material flows from nozzle118 along a direction associated with central axis 821 of fifth portionof material 810. With nozzle 118 oriented along the direction of centralaxis 821, material 800 extruded from nozzle 118 may undergo outwardspreading that is in a direction approximately perpendicular to centralaxis 821 of fifth potion of material 810. This perpendicular directionis indicated by lateral axis 820.

By adjusting the orientation of nozzle 118 to better align with acentral axis of an adjacent portion of a 3D printed structure, extrudedmaterial may build up in a direction along the central axis, rather thanbuilding up in a vertical direction or other direction that might createan undesired excess of material in various locations as the structure isformed. Although not shown, some embodiments could use supportingstructures that may provide support during formation of a structure, butwhich may be removed after the structure has been completed and is fullycured.

By moving nozzle 118 in both the vertical and horizontal direction, incombination with rotating or tilting the orientation of nozzle 118,printing system 100 and the processes described above can be used toform parts having a wide variety of geometries and shapes, includingportions with various kinds of curved surfaces. Such curved surfaces maybe constant in curvature or non-constant in curvature (e.g., compoundcurves).

Embodiments may include provisions for adjusting one or more extrusioncontrol parameters in response to feedback from sensory information. Insome embodiments, an extrusion process can adjust one or more extrusioncontrol parameters in response to optical information.

FIG. 20 illustrates an embodiment of a process for adjusting one or moreextrusion control parameters in response to optical information.Generally, one or more of the steps depicted in FIG. 20 may be performedby extrusion control system 204, sensor system 206 and/or any othersystem or component of printing device 102. In some embodiments, theprocess of FIG. 20 may include additional steps, while in otherembodiments some steps depicted in FIG. 20 may be optional. For purposesof clarity, the following discussion describes steps in this process asbeing performed by extrusion control system 204.

In a first step 902, extrusion control system 204 may receive opticalinformation. In some embodiments, the optical information may bereceived from one or more sensors, such as optical sensing device 416.The received optical information can include any kinds of analog and/ordigitals signals that include information related to one or more imagescaptured by optical sensing device 416.

In step 904, extrusion control system 204 may use the opticalinformation to characterize the outward spreading for a particularportion of material. The outward spreading of a portion of materialcould be characterized in various ways. For example, in someembodiments, the outward spreading could be characterized by thecross-sectional area, diameter, or extension along a particularpredetermined direction, of the portion of material at a given instantof time. In other embodiments, the outward spreading could becharacterized by an outward spreading rate, which is the rate at whichthe portion of material is spreading in the outward direction. Dependingon the application, it may be more useful to use either the absoluteextent of spreading of a portion of material at a particular time or therate of outward spreading of the portion of material at a particulartime. In still other embodiments, other characterizations of outwardspreading could be used. For purposes of convenience, the particularcharacterization of outward spreading used for a portion of material ata particular time is referred to as an outward spreading value.

In different embodiments, a measured or sensed outward spreading valuecould be determined using optical information. In some embodiments, oneor more images captured by optical sensing device 416 of a portion ofextruded material may analyzed to determine an absolute extent ofoutward spreading in one or more directions, and/or an outward spreadingrate. Any known algorithms for analyzing image data can be used todetermine measured or sensed values for absolute outward spreadingand/or an outward spreading rate.

In step 906, extrusion control system 204 may retrieve a predictedoutward spreading value at a given time from memory (e.g., from adatabase). In contrast to the measured or sensed outward spreadingvalue, the predicted outward spreading value is a value that ispredetermined based on assumed values of material flow rate, nozzlewithdrawal rate, extrusion temperature, as well as using possibly otherfactors. Thus, the predicted outward spreading value indicates howspreading is predicted to occur so that the desired part geometry can beachieved. The predicted outward spreading value could vary from thesensed outward spreading value due to various factors, including, butnot limited to: printed material imperfections, variations in basecomponent materials and geometries, variations in ambient conditions(e.g., temperature and pressure) as well as possibly other factors.

In step 908, the sensed outward spreading value is compared with thepredicted outward spreading value. If the sensed outward spreading valueis within a predetermined tolerance of the predicted outward spreadingvalue, the system may continue extruding material without anyadjustments. However, if the sensed outward spreading value differs fromthe predicted outward spreading value by more than a predeterminedtolerance, extrusion control system 204 may proceed to step 910 to makeadjustments to one or more extrusion control parameters.

FIG. 21 illustrates a schematic view of a process in which opticalinformation is used to provide feedback to an extrusion control system.Referring to FIG. 21, optical sensing device 416 is positioned tocapture optical information about a portion of material 1010 afterportion of material 1010 has been extruded from nozzle 118. This opticalinformation can be used to determine a sensed outward spreading diameter1022, which is a real-time measurement of the approximate diameter ofportion of material 1010 as it spreads outwardly on base component 1005.In the schematic view of nozzle 118 and portion of material 1010 of FIG.21, sensed spreading diameter 1022 of portion of material 1010 is shownfor a particular instant of time.

In the chart of FIG. 21, sensed outward spreading diameter 1022 isplotted as a function of time. Additionally, predicted outward spreadingdiameter 1020 is also plotted as a function of time. In this case,predicted outward spreading diameter 1020 follows an approximatelystraight line, which indicates a generally constant spread of materialin time (e.g., a constant spreading rate). It will be understood thatpredicted outward spreading diameter 1020 is only one exemplary type offunction, which is used here for clarity, and in other embodiments thebehavior of predicted outward spreading diameter 1020 could benon-linear.

At time T1, predicted outward spreading diameter 1020 and sensed outwardspreading diameter 1022 may be approximately the same. In other words,at this point, sensed outward spreading diameter 1022 may be within apredetermined tolerance of predicted outward spreading diameter 1020.This indicates that portion of material 1010 is spreading in the desiredmanner to form the first portion or layer of the intended 3D printedstructure. At a later time T2, however, sensed outward spreadingdiameter 1022 falls substantially below predicted outward spreadingdiameter 1020, indicating that portion of material 1010 is not spreadingin the desired manner (e.g., at the desired rate). As extrusion controlsystem 204 detects this relative drop in the sensed outward spreadingdiameter 1022, extrusion control system 204 may adjust the flow rate orextrusion rate of material 1008 to induce faster and/or more spreadingin portion of material 1010. In particular, at time T2, the flow rate isincreased from the initial flow rate 1040 (associated with time T1) to anew increased flow rate 1042. Following time T2, sensed outwardspreading diameter 1022 begins to increase and may fall once again withthe predetermined tolerance of predicted outward spreading diameter1020.

At a later time T3, sensed outward spreading diameter 1022 increasesabove predicted outward spreading diameter 1020, thereby indicating thatportion of material 1010 is flowing too rapidly and possibly extendingtoo far. Therefore, at time T3, the flow rate is adjusted to a newreduced flow rate 1044, which is a substantially lower flow rate thanboth initial flow rate 1040 (associated with time T1) and flow rate 1042(associated with time T2). Following time T3, sensed outward spreadingdiameter 1022 begins to decreased and may fall once again with thepredetermined tolerance of predicted outward spreading diameter 1020.This process may therefore be iterative, providing a means ofcontinuously adjusting the flow rate (or other extrusion controlparameter) in response to sensed optical information about how a portionof material is spreading. Moreover, though the exemplary process isshown in FIG. 21 for a specific portion of material 1010, correspondingto the lower layer of material in a printed structure, this process maybe used for all portions and layers of material in forming a printedstructure.

FIG. 22 illustrates an embodiment of a process for applying a curingcontrol device to a recently extruded portion of material in response tosensed information about the recently extruded portion of material. Instep 1102, extrusion control system 204 may received sensed informationfrom one or more sensors about the extruded portion and/or ambientconditions. Exemplary sensors that may supply information to extrusioncontrol system 204 include temperature sensors, pressure sensors, flowrate sensors, optical sensors as well as possibly other kinds ofsensors. In step 1104, extrusion control system 204 uses the sensedinformation to determine if the recently extruded portion of material iscured. For example, in some embodiments optical information could beused to determine if an extruded portion is stable or non-moving, andtherefore likely cured. If the recently extruded portion is not yetcured and it necessary to set the portion of material before extrudingmore material, a curing control device may be used to cure the portionof material directly. In this case, extrusion control system 204 movesto step 1106 to apply cooling and/or UV curing to the extruded portion.

Of course, in some embodiments, direct application of a curing controldevice to one or more portions of an extruded material to increase thespeed of curing can be done automatically, without relying on sensedinformation. In particular, as already depicted in earlier embodiments,direct curing (e.g., cooling) can be done to increase curing speed aspart of the process of forming portions with particular geometries thatmay require quick curing to remain stable during the printing process.

Embodiments can include provisions for applying three-dimensionalprinted structures that may be anchored to a base component, such as atextile material. In embodiments using an extrusion process that resultsin outward spreading of extruded material, it may be possible to induceoutward spreading of material on an opposing side of a base componentfrom the side where the nozzle is located. This may allow for thecreation of anchoring portions that might not be achievable withalternative processes that require a nozzle to pass above all locationswithin a volume associated with a printed structure.

FIGS. 23-27 illustrate schematic views of an embodiment of a process forprinting a 3D anchoring structure 1200 that is anchored directly to basecomponent 1202 as it is formed. As seen in FIGS. 23-27, the exemplaryprocess may utilize nozzle 118, base component 1202 and a moldingcomponent 1250. Nozzle 118 may be disposed on a first side 1210 of basecomponent 1202, while molding component 1250 may be disposed on a secondside 1212 of base component 1202. Moreover, to provide fluidcommunication between first side 1210 and second side 1212, basecomponent 1202 includes an opening 1214.

As seen in FIG. 24, material 1220 is extruded from nozzle 118 and flowsthrough opening 1214. With molding component 1250 in place againstsecond side 1212 of base component 1202, first portion of material 1222flows into cavity 1252 of molding component 1250. In FIG. 25, firstportion of material 1222 fills the entirety of cavity 1252. Becauseopening 1254 of cavity 1252 has a diameter 1256 (see FIG. 23), firstportion of material 1222 obtains a diameter 1223 directly adjacent tosecond side 1212 of base component 1202. Moreover, since diameter 1223of first portion of material 1222 is greater than diameter 1215 ofopening 1214, first portion of material 1222 is prevented from passingthrough opening 1214.

In FIG. 26, a second portion of material 1224 is extruded from nozzle118 and begins to spread laterally on first side 1210 of base component1202. In the FIG. 27, second portion of material 1226 is seen to obtaina diameter 1227 that is substantially larger than diameter 1215 ofopening 1214. Thus, the anchoring structure 1200 is formed in a mannersuch that anchoring structure 1200 cannot be separated from basecomponent 1202 without irreversibly damaging either base component 1202or anchoring structure 1200.

With anchoring structure 1200 formed as in the process depicted in FIGS.23-27, additional extruded material can be added to form various 3Dstructures extending away from first side 1210 of base component 1202.These structures could include any of the 3D printed structures alreadydiscussed, such as cleats, hooks, knob-like fasteners as well as otherstructures.

Anchoring of a structure may be achieved using a single aperture, orcould be accomplished using two or more apertures. The number ofapertures used could vary according to the type of base component usedas well as the geometry of the formed 3D structure.

In different embodiments, the type of molding component used could vary.For example, molding components could vary in size, cavity shape,material construction as well as in other properties. Any kinds of moldsknown in the art could be used. The type of mold used could be selectedaccording to the desired geometry of the final structure (especially thegeometry of the part on second side 1212 of base component 1202),required part sizes, temperature tolerances of the mold material, aswell as possibly other factors.

As one example of variations in a molding component, FIG. 28 illustratestwo alternative designs. Referring to FIG. 28, a first molding component1302 has a cavity 1303 with a generally rectangular geometry, as opposedto the approximately rounded (or dome-like) geometry of cavity 1252 ofmolding component 1250 in FIG. 23. Also, second molding component 1304has a cavity 1305 with a generally irregular geometry. These variationsin cavity geometry may result in corresponding variations in thegeometry of the formed 3D structures (for the portions of the structureson the side of the base component where the mold is placed).

In some other embodiments, anchoring structures could be created bypushing extruded material through a material, such as a knit, mesh orbraided fabric, which may not include distinct apertures. Such anembodiment is depicted in FIG. 29. Here, anchored structure 1400includes a first portion 1402 on first side 1410 of base component 1408,and a second portion 1404 on a second side 1412 of base component 1408.First portion 1402 and second portion 1404 are connected by extrudedmaterial portions 1420, which have been pushed through the open spacesin base component 1408.

FIG. 30 illustrates an exemplary embodiment of a printing device 102along with two different methods for holding or supporting articles thatmay receive printed structures. As seen in FIG. 30, in some embodiments,a flat upper portion 1502 may be placed on a tray 112 that is housedwithin printing device 102. In other embodiments, an assembled articleof footwear 1504 may be associated with a footwear holding device 1506,which may be inserted into printing device 102. In some embodiments,footwear holding device 1506 may be configured to present anapproximately flattened portion of article of footwear 1504 to a nozzlefor printing. An exemplary footwear holding device that could be used isdisclosed in Miller, U.S. Patent Publication Number 2014/0310891,published on Oct. 23, 2014 (now U.S. patent application Ser. No.13/868,130, filed Apr. 23, 2013) and titled “Holding Assembly forArticles,” the entirety of which application is herein incorporated byreference.

General systems and methods for printing 3D structures directly ontoportions of articles, including articles comprised of textiles aredisclosed in Jones et al., U.S. Patent Application Publication Number2014/0020192, published Jan. 23, 2014 (now U.S. patent application Ser.No. 13/553,368, filed Jul. 19, 2012), and entitled “Footwear AssemblyMethod with 3D Printing,” the entirety of which application is hereinincorporated by reference and hereafter referred to as the “3D Printing”application. In particular, the 3D printing application includes systemsand methods for printing onto textiles or base components that may nothave hydrophobic or non-wetting surfaces. The 3D printing applicationalso teaches systems and methods for printing onto irregular surfacessuch as those encountered in woven, knit, braided or other kinds offabrics or textile materials.

FIG. 31 is an isometric view of an embodiment of an article of footwear1600. As seen in FIG. 31, article of footwear 1600 includes a pluralityof 3D printed structures in the form of fasteners that may be engaged bya lace or other fastening provision. Specifically, article of footwear1600 includes a set of knob-like fasteners 1602 that have been formedusing a 3D printing process as previously discussed and shown in FIGS.7-14. Additionally, article of footwear 1600 includes a set of hookfasteners 1604 that have been formed using a 3D printing process aspreviously discussed and shown in FIGS. 15-19. Thus, it may be seen thatthe exemplary printing (specifically, extrusion) process discussed inthese embodiments can be used to form functional structures, such asfasteners, for articles of footwear and as well as other kinds ofarticles.

Embodiments can include further provisions to improve the speed offorming 3D printed structures. In some embodiments, a 3D printedstructure can be formed using two different printing processes to format least two different portions of the 3D printed structure. In somecases, for example, a first portion of a 3D printed structure may beformed using a first 3D printing process, while a second portion of the3D printed structure may be formed using a second 3D printing processthat is distinct from the first 3D printing process.

FIG. 32 illustrates a schematic view of an embodiment of a 3D printedstructure 1700, or simply structure 1700, which is attached to basecomponent 1720. In the embodiment of FIG. 32, structure 1700 has theform of a cleat for use with an article of footwear. However, in otherembodiments similar printed structures could be formed in a variety ofdifferent shapes and for different purposes. In other words, theprinciples discussed for structure 1700 are not intended to be limitedto making cleats or similar parts.

In the embodiment depicted in FIG. 32, structure 1700 is comprised oftwo different portions. In particular, structure 1700 includes an outershell portion 1702 and an inner portion 1704. As discussed in furtherdetail below, outer shell portion 1702 and inner portion 1704 may differin one or more characteristics, including size, volume, shape, material,color, as well as possibly other characteristics.

In different embodiments, the geometry of outer shell portion 1702 canvary. In some embodiments, outer shell portion 1702 may have a generallyrounded geometry. In some cases, for example, outer shell portion 1702could have a dome-like geometry. In other embodiments, outer shellportion 1702 could have a generally conical geometry. In some cases, forexample, outer shell portion 1702 could have a truncated conicalgeometry.

In at least some embodiments, outer shell portion 1702 may include oneor more openings. In some embodiments, outer shell portion 1702 couldinclude a single opening. In other embodiments, outer shell portion 1702could include two openings. In still other embodiments, outer shellportion 1702 could include three or more openings. In the embodimentdepicted in FIG. 32, outer shell portion 1702 includes a single opening1703.

In different embodiments, the location of one or more openings in outershell portion 1702 could vary. In some embodiments, one or more openingscould be disposed on a portion of outer shell portion 1702 locatedadjacent to base component 1720. In other embodiments, one or moreopenings could be disposed on a portion of outer shell portion 1702disposed furthest from base component 1720. In the embodiment depictedin FIG. 32, opening 1703 of outer shell portion 1702 is disposed at tipportion 1706 of outer shell portion 1702.

In some embodiments, outer shell portion 1702 may comprise a generallythin portion of material. In some embodiments, the thickness 1730 ofouter shell portion 1702 may be substantially less than a diameter 1731of outer shell portion 1702. Further, in some embodiments, the thickness1730 of outer shell portion 1702 may be substantially less than a height1732 (as measured from base component 1720) of outer shell portion 1702.In an exemplary embodiment, thickness 1730 of outer shell portion 1702may have a value approximately in the range between 0.01 millimeters and5 millimeters. In still other embodiments, thickness 1730 could begreater than 5 millimeters.

Inner portion 1704 may generally fill the interior region bounded byouter shell portion 1702. Therefore, the geometry of inner portion 1704may generally correspond to the geometry of outer shell portion 1702. Inembodiments where outer shell portion 1702 has an approximatelydome-like geometry, inner portion 1702 may also have a dome-likegeometry. In embodiments where outer shell portion 1702 has a conical(including truncated conical) geometry, inner portion 1704 may have asimilar conical geometry. In other embodiments, however, it iscontemplated that the interior region bounded by outer shell portion1702 does not have a geometry corresponding to the geometry of theexterior side of outer shell portion 1702. In such cases, the geometryof inner portion 1704 may generally correspond to the geometry inducedby the shape of the interior side of outer shell portion 1702.

In some embodiments, an outer shell portion may comprise a relativelysmall percentage of the total volume of a 3D printed structure while aninner portion can comprise a large percentage (at least a majority) ofthe total volume of the 3D printed structure. For example, in theembodiment of FIG. 32, outer shell portion 1702 is seen to have a firstvolume comprising a first percentage of the total volume of structure1700. Also, inner portion 1704 is seen to have a second volumecomprising a second percentage of the total volume of structure 1700. Inan exemplary embodiment, the second percentage is substantially greaterthan the first percentage, so that outer shell portion 1702 onlycomprises a small percentage of the total volume of structure 1700,while inner portion 1704 comprises a large percentage of the totalvolume of structure 1700.

Values of the first percentage and the second percentage can vary fromone embodiment to another. In some embodiments, the first percentage mayhave a value approximately in the range between 1 percent and 30percent. Correspondingly, in such embodiments, the second percentage mayhave a value approximately in the range between 70 percent and 99percent. Here it is to be understood that the total of the firstpercentage and the second percentage should equal 100 percent inembodiments where structure 1700 consists of only outer shell portion1702 and inner portion 1704.

In some embodiments, outer shell portion 1702 may be formed using afirst 3D printing process, while inner portion 1704 may be formed usinga second 3D process that is distinct from the first 3D printing process.Using different printing processes for each portion may allow forimprovements in efficiency and/or manufacturing speed. For example, thefollowing embodiments illustrate printing methods where outer shellportion 1702 is formed using a relatively slow printing process, whileinner portion 1704 is formed using a relatively faster printing process.Because inner portion 1704 comprises a majority of the volume ofstructure 1700, such printing methods may allow structure 1700 to beformed in a significantly shorter period of time than if the volume ofstructure 1700 were printed using the relatively slow printing process.

As shown in FIG. 32, in at least some embodiments, outer shell portion1702 and inner portion 1704 may be formed using different nozzles and/orprint heads. In one embodiment, outer shell portion 1702 may be formedusing a first nozzle 1740 while inner portion 1704 may be formed using asecond nozzle 1742. In some embodiments, first nozzle 1740 has a firstaperture 1741 while second nozzle 1742 has a second aperture 1742. Inone embodiment, first aperture 1741 may have a substantially smallerdiameter than second aperture 1742. With this configuration, a greatertotal volume of material may flow through second aperture 1742 thanthrough first aperture 1741 for a given interval of time.

Although some embodiments may use different nozzles to form outer shellportion 1702 and inner portion 1704, other embodiments may use a singlenozzle to form both outer shell portion 1702 and inner potion 1704. Suchan alternative embodiment is described below and shown in FIGS. 36-38.

In different embodiments, the materials comprising outer shell portion1702 and inner potion 1704 could vary. In some embodiments, outer shellportion 1702 may be comprised of a first material and inner portion 1704may be comprised of a second material. In some cases, the first materialmay be substantially identical to the second material. In other cases,the first material may be substantially different from the secondmaterial.

In different embodiments, the rigidities of the first material and thesecond material could vary. For example, when cured, the first materialforming the outer shell portion may have a first rigidity, while thesecond material forming the inner portion may have a second rigiditywhen cured. In some embodiments, the second rigidity may be greater thanthe first rigidity. As an example, in some embodiments for a cleatstructure, the first material could be a rubber to provide traction andgive to the outer shell portion, while the inner portion may be a harderplastic to provide structure and support to the cleat structure. Inother embodiments, the second rigidity could be less than the firstrigidity. As an example, in some embodiments of a cleat structure, thefirst material could be hard rubber or plastic to provide strengthand/or traction for the outer shell portion, while the second materialcould be a foam material for support and cushioning.

Of course in other embodiments still other combinations of materialscould be used. In particular, the first material and the second materialcould be selected to achieve various combinations of materials thatdiffer in properties including, but not limited to: weight, strength,cushioning, bonding compatibility with a base component as well as othermaterial properties.

FIGS. 33-35 illustrate schematic views of an embodiment of a process forforming structure 1700. As seen in FIG. 33, outer shell portion 1702 maybe formed first using first nozzle 1740. As indicated schematically,outer shell portion 1702 may be formed using a first 3D printingprocess. Specifically, the first 3D printing process includes movingfirst nozzle 1740 horizontally over base component 1720 so as to form ahorizontal layer of outer shell portion 1702 using extruded material1780. Unlike the embodiments discussed previously and shown, forexample, in FIGS. 7-14, the first 3D printing process does not involvesubstantial outward spreading of the printed (or extruded) material.Once a horizontal layer has been formed, for example printed layer 1785shown in FIG. 33, first nozzle 1740 may be raised an incremental amountin the vertical direction. At this point, as shown in FIG. 34, firstnozzle 1740 may again move in a horizontal manner to form a subsequentlayer of printed material 1787 on top of printed layer 1785.

In at least some embodiments, once outer shell portion 1702 has beenfully formed, outer shell portion 1702 could be cured prior to forminginner portion 1704. In some cases, the curing could be accomplished asouter shell portion 1702 is formed. In other cases, the curing could beaccomplished after outer shell 1702 has been formed, but before innerportion 1704 has been formed. In still other embodiments, however, outershell portion 1702 could be fully (or partially) cured after innerportion 1704 is formed.

Once outer shell portion 1702 has been formed by the first 3D printingprocess, first nozzle 1740 may be moved away from outer shell portion1702. As seen in FIG. 35, second nozzle 1742 may be moved to a positionabove opening 1703. At this point, a second 3D printing process may beused to fill interior void 1709 of outer shell portion 1702 with secondmaterial 1784. As shown in FIG. 35, the second 3D printing process mayinvolve maintaining second nozzle 1742 in a substantially fixed positionabove opening 1703 as second material 1784 is extruded or otherwisedeposited into interior void 1709. The second 3D printing process maycontinue until second material 1784 fills the entirety of interior void1709, thereby forming inner portion 1704 of structure 1700.

The first 3D printing process used to form outer shell portion 1702 andthe second 3D printing process used to form inner portion 1704 may bediffer in one or more attributes. As already mentioned, the first 3Dprinting process comprises moving first nozzle 1740 through a sequenceof positions disposed in a horizontal plane to form a horizontal layerof material. Upon the formation of a horizontal layer, first nozzle 1740may be briefly raised in the vertical direction to form a subsequenthorizontal layer. In contrast, the second 3D printing process comprisesmaintaining second nozzle 1742 at an approximately fixed vertical andhorizontal position, and extruding second material 1784 through opening1703 of outer shell portion 1702. Unlike outer shell portion 1702,therefore, inner portion 1704 is not formed via a process of printing aseries of stacked horizontal layers, but is instead formed by forcingsecond material 1784 into interior void 1709. It can therefore be seenthat the resulting geometry of outer shell portion 1702 is defined bythe tooling path taken by first nozzle 1740 during the first 3D printingprocess, while the resulting geometry of inner portion 1704 is inducedby the interior geometry of interior void 1709, and requires little tono movement of second nozzle 1742.

The first 3D printing process and the second 3D printing process mayalso be distinguished by the degree of outward spreading. The first 3Dprinting process may deposit material in very fine layers, which resultin little to no outward spreading. In particular, the degree of outwardspreading for material deposited using the first 3D printing process maybe less than 200% of the diameter of aperture 1741 of first nozzle 1740(see FIG. 32). In other words, material printed by first nozzle 1740 maynot spread to a size more than twice the diameter of first nozzle 1740.In contrast, the second 3D printing process relies on substantialoutward spreading to fill interior void 1709 of outer shell portion1702. Thus, outward spreading of material extruded from second nozzle1742 may be many times larger than the diameter of aperture 1743 ofsecond nozzle 1742 (see FIG. 32). For example, in some embodiments,portions of material may spread to diameters of at least 500% of thediameter of aperture 1743.

The exemplary process for forming structure 1700 may allow forimprovements in printing speed while maintaining precision for thegeometry of printed structures. This is accomplished by printing arelatively thin outer shell portion having any desired geometry using aprecisely controlled printing process and then filling in the interiorof the outer shell portion by quickly extruding or otherwise depositingprinted material into the interior. By forming only a thin outer shellfor the structure using the first 3D printing process and forming a bulkof the volume using the second 3D printing process, the printing time ofstructure 1700 may be decreased, as the second 3D printing process isgenerally a quicker than the first 3D printing process.

It will be understood that the process for forming outer shell portion1702 is only intended to be exemplary. In other embodiments, outer shellportion 1702 could be formed using any known 3D printing process. Someexemplary printing processes include any of those previously mentioned.

FIGS. 36-38 illustrate an alternative process for forming a 3D printedstructure 1800. Generally, the process shown in FIGS. 36-38 may besimilar in at least some respects to the process shown for FIGS. 33-35.In particular, the process of FIGS. 36-38 includes using a first 3Dprinting process and a second 3D printing process that may be different.However, in contrast to the embodiment shown in FIGS. 33-35, theembodiment depicted in FIGS. 36-38 uses a single nozzle 1840 to formboth outer shell portion 1802 and inner portion 1804 of structure 1800.Although nozzle 1840 may be used in both the first 3D printing processand the second 3D printing process, in at least some cases, the size ofaperture 1841 may be variable. Moreover, in some embodiments, otherextrusion control parameters could be adjustable. By varying the size ofaperture 1841 and/or additional extrusion control parameters, nozzle1840 may be configured to extrude printing material 1810 at asubstantially higher flow rate during the second 3D printing process.

Although FIGS. 36-38 illustrate an embodiment using a single material toform inner and outer portions of a printed structure, other embodimentscould use different materials. For example, in some embodiments,following the formation of outer shell portion 1802 by extruding a firstmaterial through nozzle 1840, a second material could be extrudedthrough nozzle 1840 to form inner portion 1804.

To ensure that an extruded material can completely fill the interiorvoid of an outer shell portion, some embodiments can include outer shellportions with two or more openings. FIG. 39 is a schematic view of anembodiment of a 3D printing structure 1900, which may be formed usingthe first 3D printing process and second 3D printing process describedabove and shown in FIGS. 33-35. In the embodiment of FIG. 39, printedstructure 1900 may include at least two openings: a first opening 1903and a second opening 1905 in outer shell portion 1902. In thisconfiguration, nozzle 1742 may initially fill first opening 1903, thenmove to a position over second opening 1905 and fill interior void 1909through second opening 1905. The use of multiple openings may facilitatethe filling of the interior void, especially for larger outer shellportions and/or outer shell portions having complex geometries.

FIGS. 40-46 illustrate a variety of different embodiments of 3D printedstructures, as well as methods for forming 3D printed structures. In theembodiment shown in FIGS. 40-41, 3D printed structure 2000 may comprisean outer shell portion 2002 and an inner portion 2004. In thisembodiment, outer shell portion 2002 may be include multiple anchoredportions 2010. In some embodiments, outer shell portion 2002 includesseven anchored portions that are secured within base component 2020.However, in other embodiments, any other number of anchored portionscould be used.

Anchored portions 2010 can be formed in any manner. In at least someembodiments, anchored portions 2010 can be formed using the printingprocess described above and shown in FIGS. 23-27. Specifically, in somecases, anchored portions 2010 may be formed by extruding material 2030through an opening 2032 in base component 2020, which is then receivedinto a molding component 2034 on an opposing side of base component2020. In some cases, this process can be used to form each of theanchored portions 2010 of structure 2000. In some cases, with anchoredportions 2010 formed, the remaining portions of outer shell portion 2002may be formed using the printing process described above and shown inFIGS. 33-34, i.e., by building up horizontal layers of outer shellportion 2002. In some embodiments, inner portion 2004 may be formedusing the printing process shown in FIG. 35, i.e., by extruding materialinto an interior of outer shell portion 2002.

The configuration shown in FIGS. 40-41 provides a structure 2000 inwhich outer shell portion 2002 is anchored to base component 2020, whileinner portion 2004 is not anchored to base component 2020. Thus, in atleast some embodiments, outer shell portion 2002 may act to retain innerportion 2004. In embodiments where inner portion 2004 is comprised of avery soft filler material that might not be suitable for creatinganchored portions (e.g., if inner portion 2004 is comprised of a verysoft foam), outer shell portion 2002 may ensure that inner portion 2004stays attached to base component 2020 and within outer shell portion2002.

Of course in other embodiments, inner portion 2004 could also beconfigured with one or more anchored portions. Using anchored portionswith outer shell portion 2002 and/or inner portion 2004 may reduce thetendency of structure 2000 to pull away or separate form base component2020, which may be especially useful for materials that are not suitablybond compatible with base component 2020 and/or for configurations wherestructure 2000 may encounter large forces (e.g., with a ground or othersurface) that might tend to stress material bonds between structure 2000and base component 2020.

FIGS. 42-43 illustrate an embodiment of a process for forming astructure 2100 with an outer shell portion 2102 and an inner portion2104. In the embodiment of FIGS. 42-43, inner portion 2104 extendsthrough opening 2103 of outer shell portion 2102 and includes anoutwardly directed anchoring portion 2130. Outwardly directed anchoringportion 2130 may be configured to attach to other components includingfasteners (such as laces, cords, etc.). As with previous embodiments,outer shell portion 2102 may be formed from a first 3D printing processthat provides the necessary precision for achieving a desired geometryfor structure 2100, while inner portion 2104 may be formed using asecond 3D process that can quickly fill the interior of outer shellportion 2102 and form outwardly directed anchoring portion 2130 viaoutward spreading of material.

FIGS. 44-46 illustrate an embodiment of a process for forming a cleatstructure 2200. In contrast to previous embodiments, the embodiment ofFIGS. 44-46 may not use an outer shell portion and an associated innerportion. Instead, as seen in FIG. 44, a base portion 2202 of cleatstructure 2200 may be formed by extruding a first material 2210 ontobase component 2220. Moreover, an outwardly extending anchoring portion2204 may be formed on top of base portion 2202. Next, a second material2212 may be extruded over outwardly extending anchoring portion 2204 inorder to form a tip portion 2230 for cleat structure 2200. In at leastone embodiment, second material 2212 is a substantially softer materialthan first material 2210 comprising base portion 2202, thereby providingimproved flexibility for gripping surfaces at tip portion 2030. In someembodiments, an optional molding member 2299 may be used to help definethe geometry of tip portion 2230 as second material 2212 is extruded orotherwise disposed over base portion 2202.

In at least some embodiments, rather than forming tip portion 2030 via3D printing, tip portion 2030 could be formed by another process andlater assembled over extending anchoring portion 2204. For example, tipportion 2030 could be a pre-formed cap that is manually placed over(e.g., assembled with) extending anchoring portion 2204. This manualassembly could be achieved if tip portion 2030 is substantially flexible(e.g., made of rubber).

FIG. 47 illustrates a schematic bottom isometric view of an embodimentof an article of footwear 2300, including an upper 2302 and a solestructure 2310. Referring to FIG. 47, article 2300 includes a pluralityof cleat structures, including cleat structure 1700 and cleat structure2200.

FIG. 48 is a schematic view of an embodiment of a nozzle control system2400, which may be used to operate a first nozzle 2402 and a secondnozzle 2404 in an independent manner. Specifically, in at least someembodiments, first nozzle 2402 and second nozzle 2404 may be actuated tomove independently of one another. In embodiments where two distinctprinting materials are used, or where it is desirable to have nozzles ofdifferent aperture diameters, first nozzle 2402 and second nozzle 2404may be used to form different portions of a structure. For example, insome embodiments, first nozzle 2402 could be used to form the outershell portion of a structure, while second nozzle 2404 could be used toform an inner portion of a structure. Likewise, in some otherembodiments, first nozzle 2402 could be used to form a base portion of astructure, while second nozzle 2404 could be used to form a top portionof the structure.

FIG. 49 is a schematic view of an embodiment of a process forcontrolling at least two nozzles that may move and print materialindependently of one another. In some embodiments, one or more of thefollowing steps could be accomplished by nozzle control system 2400. Inother embodiments, however, one or more other systems could perform oneor more of the steps. Still further, in other embodiments some of thesesteps could be optional.

In step 2502, nozzle control system 2400 may control first nozzle 2402to print a first portion of a structure. In some cases, the printingcould be done by extruding the first material. Next, in a step 2504,nozzle control system 2400 may align second nozzle 2404 with the firstportion of the structure formed using first nozzle 2402. In step 2506,nozzle control system 2400 may control second nozzle 2504 to print asecond portion of the structure. In some cases, the printing could bedone by extruding the second material.

It is contemplated that embodiments could use various methods foraligning, or registering, second nozzle 2404 with a formed first portionof material. Due to slight variations in the formed first portion due totolerances in the precision of many kinds of 3D printing processes,openings or other features in the first portion to which second nozzle2404 must be aligned, could vary slightly in their locations and/orgeometries. In at least some embodiments, therefore, sensors could beused to locate the first portion and/or particular features of the firstportion for alignment with second nozzle 2404. For example, in oneembodiment, an optical sensing device associated with second nozzle 2404can be used to determine the location of an opening or other feature ona formed first portion, using algorithms known in the art for detectingvisual features in image information. Thus, second nozzle 2404 may bealigned using feedback from the optical sensing device. In otherembodiments, any other alignment and/or registration provisions orfeatures could be used to ensure that second nozzle 2404 is properlyaligned with first portion before the second portion is printed withsecond nozzle 2404.

While various embodiments have been described, the description isintended to be exemplary, rather than limiting and it will be apparentto those of ordinary skill in the art that many more embodiments andimplementations are possible that are within the scope of theembodiments. Accordingly, the embodiments are not to be restrictedexcept in light of the attached claims and their equivalents. Also,various modifications and changes may be made within the scope of theattached claims.

We claim:
 1. A method of forming an anchored component on a base component of an article of apparel, the method comprising: positioning a first molding component having a first internal volume and a first internal width on a second side of the base component, the first molding component being positioned so that it is adjacent a first opening that extends from a first side of the base component to the second side of the base component, the second side of the base component being opposite the first side and the first internal width of the first molding component being greater than a first width of the first opening; delivering a first material onto a surface of the first side to form a first portion; delivering the first material into the first molding component through the first opening, the first material flowing into the first molding component and laterally spreading within the first molding component to fill the first internal volume of the first molding component; and removing the first molding component to provide a first anchoring portion on the second side of the base component that corresponds to the first internal volume of the first molding component, wherein the first anchoring portion and the first portion are integrally formed.
 2. The method of claim 1, wherein the first portion is bonded to the first side of the base component and the first anchoring portion is bonded to the second side of the base component.
 3. The method of claim 1, further comprising: positioning a second molding component having a second internal volume and a second internal width on the second side of the base component, the second molding component being positioned so that it is adjacent a second opening that extends from the first side of the base component to the second side of the base component, the second internal width of the second molding component being greater than a second width of the second opening; delivering the first material into the second molding component through the second opening, the first material flowing into the second molding component and laterally spreading within the second molding component to fill the second internal volume of the second molding component; and removing the second molding component to provide a second anchoring portion on the second side of the base component that corresponds to the second internal volume of the second molding component, wherein the first anchoring portion, the second anchoring portion, and the first portion are integrally formed.
 4. The method of claim 3, wherein delivering the first material onto the surface of the first side to form the first portion comprises: forming an outer shell portion with the first material on the first side.
 5. The method of claim 4, further comprising: delivering a second material into the outer shell portion to form a second portion that fills an internal volume of the outer shell portion.
 6. An article of apparel comprising: a base component having a first side, a second side, and a first opening between the first side and the second side; and a printed material that comprises a first portion on the first side of the base component, a first anchoring portion on the second side of the base component, and a first connecting portion extending through the first opening and connecting the first portion to the first anchoring portion; wherein the first anchoring portion has a width that is larger than the width of the first opening to restrict movement of the first anchoring portion through the first opening, and wherein the first portion, the first anchoring portion, and the first connecting portion are integrally formed from the printed material.
 7. The article of apparel of claim 6, wherein the first anchoring portion has a circular cross-sectional area.
 8. The article of apparel of claim 6, wherein the first portion is bonded to the first side of the base component, and the first anchoring portion is bonded to the second side of the base component.
 9. The article of apparel of claim 6, further comprising: a second opening between the first side and the second side of the base component; and the printed material comprising a second anchoring portion on the second side of the base component and a second connecting portion extending through the second opening and connecting the first portion to the second anchoring portion.
 10. The article of apparel of claim 9, wherein the printed material comprises a second portion on the first side of the base component, the second portion being formed from a different material than the first portion, and wherein the first portion comprises an outer shell portion that at least partially surrounds the second portion.
 11. The article of apparel of claim 10, wherein the outer shell portion has a first rigidity and the second portion has a second rigidity that is different from the first rigidity.
 12. The article of apparel of claim 11, wherein the second rigidity is greater than the first rigidity.
 13. The article of apparel of claim 11, wherein the second rigidity is less than the first rigidity.
 14. The article of apparel of claim 10, wherein the article of apparel is an article of footwear, the base component is a sole structure, and the first portion and second portion form a cleat structure.
 15. An article of apparel comprising: a base component having a first side, a first printed component on the first side of the base component, the first printed component having a lower portion and an upper portion, the upper portion having an outwardly extending anchoring portion that has an upper surface and a lower surface; and a second printed component received on the first printed component, the second printed component having a first portion in contact with the upper surface of the extending anchoring portion and a second portion in contact with the lower surface of the extending anchoring portion.
 16. The article of apparel of claim 15, wherein the article of apparel is an article of footwear, the base component is a sole structure, and the first printed component and the second printed component form a cleat structure.
 17. The article of apparel of claim 15, wherein the first printed component is formed of a first material and the second printed component is formed of a second material, the first material being different from the second material.
 18. The article of apparel of claim 15, wherein the second material is a more flexible material than the first material.
 19. The article of apparel of claim 15, wherein the second material is a rubber material and the first material is a plastic material.
 20. The article of apparel of claim 15, wherein the first printed component is bonded to the first side of the base component. 